EP1184575B1 - Turbofan for air conditioner - Google Patents

Turbofan for air conditioner Download PDF

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Publication number
EP1184575B1
EP1184575B1 EP01307539A EP01307539A EP1184575B1 EP 1184575 B1 EP1184575 B1 EP 1184575B1 EP 01307539 A EP01307539 A EP 01307539A EP 01307539 A EP01307539 A EP 01307539A EP 1184575 B1 EP1184575 B1 EP 1184575B1
Authority
EP
European Patent Office
Prior art keywords
turbofan
base plate
air
blades
shroud
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP01307539A
Other languages
German (de)
French (fr)
Other versions
EP1184575A2 (en
EP1184575A3 (en
Inventor
Nee Young Lee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
LG Electronics Inc
Original Assignee
LG Electronics Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from KR1020000052278A external-priority patent/KR20020019154A/en
Priority claimed from KR10-2000-0052277A external-priority patent/KR100389395B1/en
Priority claimed from KR10-2001-0021435A external-priority patent/KR100420355B1/en
Application filed by LG Electronics Inc filed Critical LG Electronics Inc
Publication of EP1184575A2 publication Critical patent/EP1184575A2/en
Publication of EP1184575A3 publication Critical patent/EP1184575A3/en
Application granted granted Critical
Publication of EP1184575B1 publication Critical patent/EP1184575B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/40Organic materials
    • F05D2300/43Synthetic polymers, e.g. plastics; Rubber

Definitions

  • the present invention relates to a turbofan and more particularly, to an improved turbofan for an air conditioner.
  • FIG. 1 illustrates a perspective disassembled view of a related art window air conditioner, referring to which the related art window air conditioner will be explained.
  • the front grill 3 is provided with an inlet 3i in a lower part thereof for drawing room air, and an outlet grill 3e in an upper part thereof for discharging the air heat exchanged in the air conditioner into the room, again.
  • an inlet grill (not shown) provided to the inlet 3i, and a filter (not shown) between the inlet grill and the inlet 3i.
  • an air guide 7 at an inner side of the front grill 3 provided with a room heat exchanger 5, for cooling the air drawn through the inlet 3i by heat exchange between working fluids in an air conditioning cycle.
  • the air guide 7 is fitted to an upper surface of the base pan 1, and partitions the air conditioner into an indoor side and an outdoor side. That is, the indoor side and the outdoor side are isolated by the air guide 7 to cut off air circulation between the two.
  • the air guide 7 has a shaft hole 7' for pass of a shaft of a motor 15 for rotating the sirocco fan 13.
  • the air guide 7 has a control box hold 8 formed as one unit with the air guide 7 at one side thereof for holding a control box (not shown) therein.
  • a scroll 9 fitted in the air guide 7.
  • the scroll 9 has a flow guide surface 9g form inside thereof with a required curvature from one side to the other side.
  • a back of middle part of the outlet guide 11e is opened, at both ends of which opening coupling parts 11' are formed for coupling with the top of the air guide 7.
  • the sirocco fan 13 fitted in the scroll 9 makes room air to flow through the inlet 3 i, the indoor heat exchanger 5, and the orifice hole 12.
  • the sirocco fan 13 draws air through the orifice 12, and leads the air to flow in a circumferential direction thereof along the flow guide surface 9g to the outlet guide 11e.
  • the motor 15 in the outdoor side (rear side) of the air guide 7 for rotating the sirocco fan 13 and the fan 17.
  • the motor 15 has a shaft projected in front and back thereof, one of which is passed through the air guide 7, projected up to a center of the scroll 9, and coupled with the sirocco fan 13.
  • the fan 17 is coupled to the outdoor side shaft of the motor 15.
  • the fan 17 draws air from outside of the air conditioner, and makes the air to pass through the indoor heat exchanger 19.
  • the fan 17 has a ring 17r connected at ends of blades.
  • the window air conditioner is installed such that the indoor side of the window air conditioner is in an air conditioning-space, and the outdoor side is in the outdoor.
  • the air conditioning cycle is activated, as the motor 15 rotates the sirocco fan 13 and the fan 17.
  • indoor side air is provided to the indoor heat exchanger 5 through the inlet 3i.
  • the heat exchanged air is provided to the sirocco fan 13 through the orifice hole 12.
  • the air drawn into the sirocco fan 13 is guided in the circumferential direction of the sirocco fan 13, until the air is discharged therefrom, guided along the flow guide surface 9g of the scroll 9, lead to the outlet guide 11e, and discharged to the air conditioning space again through the outlet grill 3e.
  • the sirocco fan 13, used for drawing the room air is designed for handling a large volume of air, has numerous short blades each having a curvature opposite to a direction of rotation to require a separate air guide structure, the scroll 9, for forming an air flow.
  • the use of scroll causes various problems.
  • the air is discharged in the circumferential direction of the sirocco fan 13 throughout the flow guide surface 9g. Therefore, the air discharged in an upstream of the flow guide surface 9g keeps to flow along the flow guide surface 9g, to build up a higher air pressure as the air flows to a downstream the farther to act as a resistance against the rotation of the sirocco fan 13.
  • FIGS. 2 , 3A, and 3B An example of a related art turbo fan will be explained with reference to FIGS. 2 , 3A, and 3B .
  • the related art turbo fan is provided with a base plate 32 of a circular disc having a hub 38 at a center thereof for coupling with a shaft of a motor, a plurality of blades 34 fitted along a circumference of the base plate 32, and a shroud 36 formed as a unit with the blades 34.
  • the blade 34 has a blade exit angle ⁇ 2 smaller than 90°, a ratio of inside/outside diameters smaller than 0.8, a backward curved form, and an inlet width W1 into which the air is started to be introduced thereto smaller than an outlet width W2.
  • the shroud 36 is annular to connect all blades 34 at a side widths of the blades 34 are smaller.
  • the shroud 36 guides the air flowing along the blade 34, and makes the air flowing between adjacent blades discharged from the blades 34 at a required pressure.
  • a blade inlet angle ⁇ 1 on the hub 38 and the blade exit angle ⁇ 2 on the shroud side 36 may differ for producing a uniform flow between the blades 34, and improve noise characteristics.
  • the turbofan requires no additional flow guide surface in view of operation of the turbofan, the turbofan facilitates omission of the scroll 9 in FIG. 9 , to permit to make an overall structure of the air conditioner simple.
  • the base plate 32 and the blades 34 are injection molded of plastic as one unit, and the shroud 36 is also injection molded of plastic separate from the base plate and the blades.
  • the shroud 36 is then fusion welded to the blades 34 by an ultrasonic wave.
  • a structure of the foregoing related art turbofan has the following demerits.
  • the structure of the related art turbofan does not permit a unitary injection molding of the shroud 36, the base plate 32, and the blades 34, so as to require the shroud 36 formed as a separate unit to weld onto the unitary base plate 32 and the blades 34 by ultrasonic wave, of which alignment of the two units for the welding is not easy to cause a high defect ratio.
  • ultrasonic wave of which alignment of the two units for the welding is not easy to cause a high defect ratio.
  • the related art turbofan has the outlet width W2 smaller than the inlet width W1, implying that a flow area ratio of the discharged air by the blade 34 differ at the inlet and the outlet, i.e., the flow area of the discharge air becomes the smaller as it goes from the inlet to the outlet of the blade 34.
  • Such a difference of the flow areas of the blade 34 also induces a difference of discharge air pressures, to cause imbalance of the pressures, that in turn causes flow noise.
  • FIG. 4 illustrates a structure of turbofan that overcomes a structural limitation that the shroud 36 and the base plate 32 and the blades 34 can not be injection molded as a unit, one of problems of the related art turbofan.
  • the turbofan is provided with a base plate 42 having a boss 41 at a center thereof for coupling with a shaft (not shown) of a motor, and a plurality of blades 43 formed in a radial direction centered on the boss 41 along a periphery of the base plate 42.
  • a shroud 44 at a side of the blades 43 opposite to the base plate 42.
  • the shroud 44 has an inside diameter D equal to, or greater an outside diameter D2 of the base plate 42, and an inlet side end 44a parallel to a shaft direction.
  • the foregoing structure is provided, for preventing interferences between molds when an upper mold 'A' and a lower mold 'B' are separated along a parting line 'G', thereby forming the boss 41, the base plate 42, and the shroud 44 at a time as one unit.
  • the shroud 44 is curved outward as it goes from the inlet side end 44a to the outlet of the blades 43, to form a curved part 44b as shown in FIG. 4 .
  • a depth of a step 44c formed in a radial direction in an inside circumference of the inlet side end 44a can not but be smaller than a radial direction thickness 't' of the shroud 44.
  • turbofan formed thicker than a certain limit for an example, 4mm
  • a certain limit for an example, 4mm
  • the depth ⁇ of the step 44c is only 1 mm - 2mm.
  • the depth ⁇ of the step 44c can not but be smaller than the thickness of the turbofan, wherein, though the injection molding is done well initially, a burr may be formed at the step 44c of the turbofan after completion of the injection molding since a part of the lower mold for the step 44c wears down to form a sharp edge after a prolonged use of the mold. That is, a lifetime of the mold is shortened due to the easy wear down of the part for the step 44c of the turbofan. Moreover, since the depth of the step 44c is smaller than the radial direction thickness 't' of the shroud 44, formation of the mold is not easy.
  • the foregoing related art turbofan has an unstable flow characteristics because of vortices formed on outer side of the curved shroud 44, that causes noise if a difference of discharge flow speeds coming from the form of the shroud 44 affects an air flow and turbulence inside of the casing 51.
  • EP 0 926 452 describes an air conditioner having a centrifugal fan for radially blowing off air sucked in.
  • the centrifugal fan has a shroud with an annular guide portion which is provided radially outside a blade support portion and a cylindrical mouthpiece portion curved and extending toward the suction side in the axial direction.
  • EP 0 791 788 describes an air conditioner with an air blow fan with a shroud.
  • US 5511 939 describes a multi-blade fan device having bottom plate with an axially separated shroud member that has an inner surface that is located on the same radius as that of the outer periphery of the bottom plate.
  • the present invention seeks to address one or more of the problems due to limitations and disadvantages of the related art.
  • turbofan for an air conditioner, which facilitates unitary formation of a turbofan, and easy formation of a turbofan mold, and has a longer lifetime of the mold.
  • turbofan for an air conditioner; which can minimize noise produced during operation of the turbofan.
  • the invention provides a turbofan in an air conditioner which includes a base plate having a hub at a center thereof, the hub-coupled to a shaft of a driving motor, a plurality of blades disposed at a periphery of the base plate at fixed intervals along a circumferential direction, and a shroud including an inlet side end part formed in parallel to the shaft, and fitted to ends of the blades 40 to connect the ends, having an inside diameter equal to, or greater than an outside diameter of the base plate, a shoulder part extended outward in a radial direction from an inside circumference of the inlet side end part, and a sloped part extended outward in a radial direction, and sloped downward, from an end of the shoulder part
  • the base plate includes a central part having the hub formed like a cap so that the central part is disposed near to an inlet compared to a bottom part thereof on an outer side of the central part, and a connecting part between the central part having the hub and the bottom part having a plurality of openings along a circumference thereof
  • the connecting part is parallel with a direction of the shaft, wherein a part where the central part and the connecting part meet is curved.
  • the shoulder part has a at least 4mm width.
  • air flow through the turbofan is made smooth to reduce noise relative to other forms of turbofan having the same air flow rate, and a lifetime of a mold is prolonged as formation of the mold is easy and wear can be inhibited Moreover, unitary formation of the entire turbofan at a time by injection molding is made possible.
  • a turbofan in a window air conditioner including a base plate having a hub at a center thereof for coupling to a shaft of a driving motor, a plurality of blades disposed on an outside circumference of the base plate at fixed intervals along a circumferential direction, and a shroud fitted to ends of the blades
  • the outside circumference of the base plate fitted to inside surface of the blades is fitted to the blades in a state the outside circumference of the base plate is bent forward or backward of the turbofan.
  • the outside circumference of the base plate is bent forward or backward of the turbofan by 90°.
  • the inside surfaces of the blades fitted to the shroud are positioned nearer to a center side of the turbofan than an inside circumference of a fore end of the shroud.
  • -A turbofan in a window air conditioner including a base plate having a hub at a center thereof for coupling to a shaft of a driving motor, a plurality of blades each having identical inlet width and outlet width disposed at a periphery of the base plate along a circumferential direction, and a shroud fitted to ends of the blades.
  • the shroud includes a connecting part for connecting a turbofan front side fore end of each blade, and a shoulder part extended perpendicular to the connecting part from an inside end of the connecting part toward a front side of the turbofan.
  • the connecting part of the shroud is fitted to an entire fore end of the blade, or only to a part of the fore end of the blade.
  • the unitary formation of the entire turbofan by injection molding permitted by aspects - of the present invention facilitates an easy formation of mold, and inhibits wear of the mold, to prolong a lifetime of the mold.
  • -A turbofan in a window air conditioner including a base plate projected forward to the shroud side in two stages having a hub at a projected center thereof for coupling to a shaft of a driving motor, a plurality of blades each having identical inlet width and outlet width disposed at a periphery of the base plate at fixed intervals along a circumferential direction, and a shroud fitted to ends of the blades.
  • Shaft direction widths of the turbofan and the motor can be reduced, to secure a larger space for adjacent components to give more freedom in arranging and designing the adjacent components.
  • the unitary formation of the entire turbofan by injection molding permitted by further aspect of the present invention facilitates an easy formation of mold, and inhibits wear of the mold, to prolong a lifetime of the mold.
  • the blade has a streamlined or planar section.
  • FIG. 7 illustrates a perspective view of a turbofan for use in a window air conditioner in accordance with a first preferred embodiment of the present invention
  • FIG. 8 illustrates a section of the turbofan in FIG. 7
  • FIG. 9 illustrates an enlarged view of key parts of the turbofan in FIG. 7
  • FIG. 10 illustrates a section showing an air flow when the turbofan in accordance with a first preferred embodiment of the present invention is applied thereto.
  • the turbofan in a window air conditioner in accordance with a first preferred embodiment of the present invention includes a base plate 30 having a hub 32 at a center thereof for coupling to a shaft of a driving motor, a plurality of blades 40 disposed at a periphery of the base plate 30 at fixed intervals along a circumferential direction, and a shroud 50 having an inlet side end part 52 formed in parallel to the shaft, fitted to ends of the blades 40 to connect the ends, with an inside diameter D1 equal to, or greater than an outside diameter D2 of the base plate 30, a shoulder part 54 extended outward in a radial direction from an inside circumference of the inlet side end part 52, and a sloped part 56 extended outward in a radial direction, and sloped downward, from an end of the shoulder part 54.
  • the base plate 30 has a central part with the hub 32 formed like a cap so that the central part is disposed near to an inlet compared to a bottom part 31 thereof on an outer side of the central part, for balancing a weight of the turbofan, wherein a connecting part 36 between the central part having the hub 32 and the bottom part 31 has a plurality of openings 38 along a circumference thereof for smooth discharge of a heat generated at the motor. It is preferable that a part the central part with the hub and the connecting part meet is curved, while the connecting part 36 is parallel to the shaft. A width of the shoulder part 54 of the shroud 50 is designed to be at least 4mm.
  • a mold for forming the turbofan in accordance with a first preferred embodiment of the present invention, and works of the turbofan formed from the mold will be explained.
  • the base plate 30, the blades 40, and the shroud 50 of the turbofan of the present invention are formed as one unit.
  • a part that causes the greatest problem in the molds 'A' and 'B' of the foregoing structured turbofan is the shroud part 50. Therefore, as shown in FIG. 9 , the upper mold 'A' is fitted such that the upper mold 'A' can be drawn through an inside diametral surface of the inlet side end part 52 of the shroud 50 after the turbofan is formed, and the lower mold 'B' is fitted such that the lower mold 'B' can be drawn to a lower side of the shoulder part 54 and the sloped part 56 along an out side diameter of the base plate 30 after the turbofan is formed. That is, a parting line of the molds is either on an outside diameter D2 of the base plate 30, or on an inside circumference of the inlet side end part 52 which has a greater diameter than the outside diameter D2.
  • the first preferred embodiment of the present invention permits to form the entire turbofan as one unit by one time of injection molding, since there is no overlapped part between the shroud 50 and the base plate 30, permitting to minimizing the defect ratio occurred in formation of the turbofan, that improves a productivity.
  • the hub 32 on the base plate 30 disposed at a center part both in an axis direction and the radial direction can balance the turbofan, to allow stable and safe dismantling of the mold in formation of the turbofan, that prevents distortion of the turbofan.
  • the hub 32 at a center both in the axis direction and the radial direction permits to maintain balance when the hub is coupled to the shaft of the motor, such that the turbofan rotates accurately without eccentricity, which reduces vibration and noise.
  • the shroud 50 has the inlet side end part 52 parallel to the rotation axis, the shoulder part 54 extended outward from the inlet side end part 52 parallel to the base plate 30, and the sloped part 56 extended outward, and sloped with respect to the base plate 30, from a fore end the shoulder part 54. That is, the shoulder part 54 is annular with a depth 5 outwardly from the inlet side end part 52, to form a diameter D4 of an outer end of the shoulder part to be at least greater than an outside diameter D3 of the inlet side end part 52 of the shroud 50.
  • the turbofan in accordance with a first preferred embodiment of the present invention has flow characteristics as shown in FIG. 10 owing to this configuration, resulting to reduce noise. That is, a noise caused by turbulence occurred at the shroud 50 is reduced.
  • FIG. 10 illustrates an LDV experiment for visualizing a flow characteristic of the turbofan of the present invention, wherein a size of the turbulence occurred at the shroud 50 of the turbofan and characteristics of a discharge flow are shown. That is, the turbofan in accordance with a first preferred embodiment of the present invention has a good air flow characteristics, and especially, no vortex at the discharge side as shown in FIG. 10 owing to a configuration of the shroud 50.
  • the turbofan of the present invention has lower noise if the air flow rates are the same.
  • the greater death ' ⁇ ' of the shoulder part 54 which leads a width of a part of the lower mold 'B' for the shoulder 54 to be greater too, not only facilitates an easier fabrication of the molds 'A' and 'B' than the related art, but also inhibits wear to the maximum, to prolong the lifetime. That is, since the fist embodiment turbofan of the present invention can reduce noise for the same air flow rate, permit an easy formation of the molds; and inhibit wear relative to the related art, a lifetime of the molds can be increased.
  • FIGS. 11A and 11B illustrate sections of blades applicable to the embodiments of the present invention.
  • the blades 40 and 60 of the turbofan in different embodiments of the present invention may have a streamlined section as shown in FIG. 11A , or a simple planar section as shown in FIG. 11B .
  • the turbofan in a window air conditioner of the present invention has the following advantages.
  • Unitary formation of a turbofan is facilitated to minimize a ratio of defects occurred in formation of the turbofan and to improve a productivity, an easy formation of a turbofan mold is made possible, and a lifetime of the mold is prolonged. Vibration and noise occurred during operation of the turbofan can be minimized.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Air-Conditioning Room Units, And Self-Contained Units In General (AREA)

Description

    BACKGROUND OF THE INVENTION Field of the Invention
  • The present invention relates to a turbofan and more particularly, to an improved turbofan for an air conditioner.
  • Background of the Related Art
  • FIG. 1 illustrates a perspective disassembled view of a related art window air conditioner, referring to which the related art window air conditioner will be explained.
  • There is a front grill 3 at a front face (indoor side) of a base pan 1, a bottom of the air conditioner. The front grill 3 is provided with an inlet 3i in a lower part thereof for drawing room air, and an outlet grill 3e in an upper part thereof for discharging the air heat exchanged in the air conditioner into the room, again. There is an inlet grill (not shown) provided to the inlet 3i, and a filter (not shown) between the inlet grill and the inlet 3i.
  • There is an air guide 7 at an inner side of the front grill 3 provided with a room heat exchanger 5, for cooling the air drawn through the inlet 3i by heat exchange between working fluids in an air conditioning cycle. The air guide 7 is fitted to an upper surface of the base pan 1, and partitions the air conditioner into an indoor side and an outdoor side. That is, the indoor side and the outdoor side are isolated by the air guide 7 to cut off air circulation between the two. The air guide 7 has a shaft hole 7' for pass of a shaft of a motor 15 for rotating the sirocco fan 13. There is also a brace 7B at a top of the air guide 7 formed as a unit with the air guide 7 for fastening to a shroud 18 of a fan. The air guide 7 has a control box hold 8 formed as one unit with the air guide 7 at one side thereof for holding a control box (not shown) therein. There is a scroll 9 fitted in the air guide 7. The scroll 9 has a flow guide surface 9g form inside thereof with a required curvature from one side to the other side. There is an orifice 11 fitted in front of the scroll 9, with an orifice hole 12 for guiding the air flowing through the indoor heat exchanger 5 toward the sirocco fan 13. There is an outlet guide 11e formed as a unit with the orifice 11 at a top of the orifice 11 for guiding the heat exchanged air toward the outlet grill 3e. A back of middle part of the outlet guide 11e is opened, at both ends of which opening coupling parts 11' are formed for coupling with the top of the air guide 7. There is a finger guide `F' at a back of the outlet guide 11e for cutting off access to the sirocco fan 13 from an outside. There is a projection 'E' formed of ESP at one side of the outlet guide 11e for preventing the white scroll 9 from being seen from outside. Since the outlet guide 11e is formed above the orifice 11, the orifice 11 is inserted between the indoor heat exchanger 5 and the sirocco fan 13 from above. That is, the orifice 11 is assembled in a top-down method. The sirocco fan 13 fitted in the scroll 9 makes room air to flow through the inlet 3 i, the indoor heat exchanger 5, and the orifice hole 12. The sirocco fan 13 draws air through the orifice 12, and leads the air to flow in a circumferential direction thereof along the flow guide surface 9g to the outlet guide 11e.
  • The explanation made up to now is on the indoor side of the window air conditioner, and the outdoor side of the window air conditioner will be explained.
  • There is a motor 15 in the outdoor side (rear side) of the air guide 7 for rotating the sirocco fan 13 and the fan 17. The motor 15 has a shaft projected in front and back thereof, one of which is passed through the air guide 7, projected up to a center of the scroll 9, and coupled with the sirocco fan 13. The fan 17 is coupled to the outdoor side shaft of the motor 15. The fan 17 draws air from outside of the air conditioner, and makes the air to pass through the indoor heat exchanger 19. The fan 17 has a ring 17r connected at ends of blades. There is a fan shroud 18 fitted on the base pan 1 for guiding air flow formed by the fan 17, having an opening 18' in communication with an outdoor heat exchanger 19 side for fitting the fan 17 therein. There is an outdoor heat exchanger 19 on outdoor side of the base pan 1 opposite to the fan shroud 18. Though not shown, there are a compressor and an expansion valve and the like, elements of the air conditioning cycle, on the outdoor side. Lastly, the different components of the air conditioner are enclosed by an outer case 20. The outer case 20 forms an outer appearance of the air conditioner. The window air conditioner is installed such that the indoor side of the window air conditioner is in an air conditioning-space, and the outdoor side is in the outdoor.
  • The operation of the air conditioner will be explained.
  • Upon putting the air conditioner into operation, the air conditioning cycle is activated, as the motor 15 rotates the sirocco fan 13 and the fan 17. According to this, indoor side air is provided to the indoor heat exchanger 5 through the inlet 3i. The air heat exchanges with a working fluid as the air passes through the heat exchanger 5, to be cooled down to a relatively low temperature. The heat exchanged air is provided to the sirocco fan 13 through the orifice hole 12. The air drawn into the sirocco fan 13 is guided in the circumferential direction of the sirocco fan 13, until the air is discharged therefrom, guided along the flow guide surface 9g of the scroll 9, lead to the outlet guide 11e, and discharged to the air conditioning space again through the outlet grill 3e.
  • On the other hand, in the outdoor side, an operation for discharging a heat, the working fluid is received at the indoor heat exchanger 5, is in process. That is, external air is drawn by the fan 17, heat exchanged with the outdoor heat exchanger 19, for discharging the heat to outside of the room.
  • However, the related art window air conditioner has the following problems.
  • First, the sirocco fan 13, used for drawing the room air, is designed for handling a large volume of air, has numerous short blades each having a curvature opposite to a direction of rotation to require a separate air guide structure, the scroll 9, for forming an air flow. However, the use of scroll causes various problems. In detail, the air is discharged in the circumferential direction of the sirocco fan 13 throughout the flow guide surface 9g. Therefore, the air discharged in an upstream of the flow guide surface 9g keeps to flow along the flow guide surface 9g, to build up a higher air pressure as the air flows to a downstream the farther to act as a resistance against the rotation of the sirocco fan 13. Moreover, since the air is concentrated to the downstream of the flow guide surface 9g, the air flows concentrated on one side of the outlet guide 11e. At the end, in view of the whole outlet grill 3e, the air is not discharged from the outlet grill 3e, uniformly. Accordingly, in order to solve the demerit of the sirocco fan designed for handling a large volume of air, a technology is suggested, in which a high efficiency turbofan is employed for forming an indoor air flow.
  • An example of a related art turbo fan will be explained with reference to FIGS. 2, 3A, and 3B.
  • The related art turbo fan is provided with a base plate 32 of a circular disc having a hub 38 at a center thereof for coupling with a shaft of a motor, a plurality of blades 34 fitted along a circumference of the base plate 32, and a shroud 36 formed as a unit with the blades 34. The blade 34 has a blade exit angle β2 smaller than 90°, a ratio of inside/outside diameters smaller than 0.8, a backward curved form, and an inlet width W1 into which the air is started to be introduced thereto smaller than an outlet width W2. The shroud 36 is annular to connect all blades 34 at a side widths of the blades 34 are smaller. The shroud 36 guides the air flowing along the blade 34, and makes the air flowing between adjacent blades discharged from the blades 34 at a required pressure. A blade inlet angle β1 on the hub 38 and the blade exit angle β2 on the shroud side 36 may differ for producing a uniform flow between the blades 34, and improve noise characteristics. As the turbofan requires no additional flow guide surface in view of operation of the turbofan, the turbofan facilitates omission of the scroll 9 in FIG. 9, to permit to make an overall structure of the air conditioner simple.
  • A process for fabricating the related art turbofan will be explained. The base plate 32 and the blades 34 are injection molded of plastic as one unit, and the shroud 36 is also injection molded of plastic separate from the base plate and the blades. The shroud 36 is then fusion welded to the blades 34 by an ultrasonic wave.
  • However, a structure of the foregoing related art turbofan has the following demerits. At first, the structure of the related art turbofan does not permit a unitary injection molding of the shroud 36, the base plate 32, and the blades 34, so as to require the shroud 36 formed as a separate unit to weld onto the unitary base plate 32 and the blades 34 by ultrasonic wave, of which alignment of the two units for the welding is not easy to cause a high defect ratio. Because an exact alignment of the two units before the welding, as well as prevention of misalignment caused by vibration, and deformation of the blades 34, during the welding are required, elimination of defects in the fabrication process has not been easy. Also, there has been a burden of expense for providing an expensive equipment, such as an ultrasonic welder, for fabrication of the related art turbofan, that pushes up a production cost of the turbofan.
  • Referring to FIG. 3B, the related art turbofan has the outlet width W2 smaller than the inlet width W1, implying that a flow area ratio of the discharged air by the blade 34 differ at the inlet and the outlet, i.e., the flow area of the discharge air becomes the smaller as it goes from the inlet to the outlet of the blade 34. Such a difference of the flow areas of the blade 34 also induces a difference of discharge air pressures, to cause imbalance of the pressures, that in turn causes flow noise.
  • In the meantime, FIG. 4 illustrates a structure of turbofan that overcomes a structural limitation that the shroud 36 and the base plate 32 and the blades 34 can not be injection molded as a unit, one of problems of the related art turbofan.
  • Referring to FIG. 4, the turbofan is provided with a base plate 42 having a boss 41 at a center thereof for coupling with a shaft (not shown) of a motor, and a plurality of blades 43 formed in a radial direction centered on the boss 41 along a periphery of the base plate 42. There is a shroud 44 at a side of the blades 43 opposite to the base plate 42. The shroud 44 has an inside diameter D equal to, or greater an outside diameter D2 of the base plate 42, and an inlet side end 44a parallel to a shaft direction.
  • Referring to FIG. 5, the foregoing structure is provided, for preventing interferences between molds when an upper mold 'A' and a lower mold 'B' are separated along a parting line 'G', thereby forming the boss 41, the base plate 42, and the shroud 44 at a time as one unit. The shroud 44 is curved outward as it goes from the inlet side end 44a to the outlet of the blades 43, to form a curved part 44b as shown in FIG. 4.
  • However, the foregoing related art turbofan has the following problems.
  • First, a depth of a step 44c formed in a radial direction in an inside circumference of the inlet side end 44a can not but be smaller than a radial direction thickness 't' of the shroud 44. as turbofan formed thicker than a certain limit (for an example, 4mm) pushes up cost, and has a poor quality due to shrinkage during formation, so as to form the turbofan below a certain thickness. Accordingly, for an example, if the thickness of the turbofan is 4mm, the depth β of the step 44c is only 1 mm - 2mm. Thus, the depth β of the step 44c can not but be smaller than the thickness of the turbofan, wherein, though the injection molding is done well initially, a burr may be formed at the step 44c of the turbofan after completion of the injection molding since a part of the lower mold for the step 44c wears down to form a sharp edge after a prolonged use of the mold. That is, a lifetime of the mold is shortened due to the easy wear down of the part for the step 44c of the turbofan. Moreover, since the depth of the step 44c is smaller than the radial direction thickness 't' of the shroud 44, formation of the mold is not easy.
  • In the meantime, referring to FIG. 6, the foregoing related art turbofan has an unstable flow characteristics because of vortices formed on outer side of the curved shroud 44, that causes noise if a difference of discharge flow speeds coming from the form of the shroud 44 affects an air flow and turbulence inside of the casing 51.
  • EP 0 926 452 describes an air conditioner having a centrifugal fan for radially blowing off air sucked in. The centrifugal fan has a shroud with an annular guide portion which is provided radially outside a blade support portion and a cylindrical mouthpiece portion curved and extending toward the suction side in the axial direction.
    EP 0 791 788 describes an air conditioner with an air blow fan with a shroud.
    US 5511 939 describes a multi-blade fan device having bottom plate with an axially separated shroud member that has an inner surface that is located on the same radius as that of the outer periphery of the bottom plate.
  • SUMMARY OF THE Invention
  • The present invention seeks to address one or more of the problems due to limitations and disadvantages of the related art.
  • It would be desirable to provide a turbofan for an air conditioner, which facilitates unitary formation of a turbofan, and easy formation of a turbofan mold, and has a longer lifetime of the mold.
  • It would also be desirable to provide a turbofan for an air conditioner; which can minimize noise produced during operation of the turbofan.
  • Additional features and advantages of the invention will be set forth in the description which follows, and in part will be apparent from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention will be realized and attained by the structure particularly pointed out in the written description and claims hereof as well as the appended drawings.
  • The invention provides a turbofan in an air conditioner which includes a base plate having a hub at a center thereof, the hub-coupled to a shaft of a driving motor, a plurality of blades disposed at a periphery of the base plate at fixed intervals along a circumferential direction, and a shroud including an inlet side end part formed in parallel to the shaft, and fitted to ends of the blades 40 to connect the ends, having an inside diameter equal to, or greater than an outside diameter of the base plate, a shoulder part extended outward in a radial direction from an inside circumference of the inlet side end part, and a sloped part extended outward in a radial direction, and sloped downward, from an end of the shoulder part
  • Preferably, the base plate includes a central part having the hub formed like a cap so that the central part is disposed near to an inlet compared to a bottom part thereof on an outer side of the central part, and a connecting part between the central part having the hub and the bottom part having a plurality of openings along a circumference thereof
  • Preferably, the connecting part is parallel with a direction of the shaft, wherein a part where the central part and the connecting part meet is curved.
  • Preferable, the shoulder part has a at least 4mm width.
  • In embodiment of the invention, air flow through the turbofan is made smooth to reduce noise relative to other forms of turbofan having the same air flow rate, and a lifetime of a mold is prolonged as formation of the mold is easy and wear can be inhibited Moreover, unitary formation of the entire turbofan at a time by injection molding is made possible.
  • There is provided a turbofan in a window air conditioner including a base plate having a hub at a center thereof for coupling to a shaft of a driving motor, a plurality of blades disposed on an outside circumference of the base plate at fixed intervals along a circumferential direction, and a shroud fitted to ends of the blades
  • Preferably, the outside circumference of the base plate fitted to inside surface of the blades is fitted to the blades in a state the outside circumference of the base plate is bent forward or backward of the turbofan.
  • Preferably, the outside circumference of the base plate is bent forward or backward of the turbofan by 90°.
  • Preferably, the inside surfaces of the blades fitted to the shroud are positioned nearer to a center side of the turbofan than an inside circumference of a fore end of the shroud.
  • In embodiments of the invention, since there is no overlapped part between the shroud and the base plate, unitary formation of the entire turbofan at a time by injection molding is made possible, and an adequate width of the connecting part connecting outside circumference of the base plate and inside surface of the blade can be secured. Moreover, since unitary formation of the entire turbofan at a time by inflection molding is made possible, formation of the mold becomes easy, and a lifetime of the mold is prolong as wear of the mold can be inhibited.
  • -A turbofan in a window air conditioner including a base plate having a hub at a center thereof for coupling to a shaft of a driving motor, a plurality of blades each having identical inlet width and outlet width disposed at a periphery of the base plate along a circumferential direction, and a shroud fitted to ends of the blades.
  • Preferably, the shroud includes a connecting part for connecting a turbofan front side fore end of each blade, and a shoulder part extended perpendicular to the connecting part from an inside end of the connecting part toward a front side of the turbofan.
  • Preferably, the connecting part of the shroud is fitted to an entire fore end of the blade, or only to a part of the fore end of the blade.
  • Since there is a uniform air pressure from a blade inlet to a blade outlet, to make a pressure balance, air flow noise is suppressed to the maximum.
  • The unitary formation of the entire turbofan by injection molding permitted by aspects - of the present invention facilitates an easy formation of mold, and inhibits wear of the mold, to prolong a lifetime of the mold.
  • -A turbofan in a window air conditioner including a base plate projected forward to the shroud side in two stages having a hub at a projected center thereof for coupling to a shaft of a driving motor, a plurality of blades each having identical inlet width and outlet width disposed at a periphery of the base plate at fixed intervals along a circumferential direction, and a shroud fitted to ends of the blades.
  • Shaft direction widths of the turbofan and the motor can be reduced, to secure a larger space for adjacent components to give more freedom in arranging and designing the adjacent components.
  • The unitary formation of the entire turbofan by injection molding permitted by further aspect of the present invention facilitates an easy formation of mold, and inhibits wear of the mold, to prolong a lifetime of the mold.
  • Preferably, the blade has a streamlined or planar section.
  • It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are intended to provide further explanation of the invention as claimed.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention:
    • In the drawings:
      • FIG. 1 illustrates a perspective disassembled view of a related art window air conditioner;
      • FIG. 2 illustrates a perspective view of a related art turbofan for use in a window air conditioner;
      • FIG. 3A illustrates a front view of the related art turbofan in FIG. 2;
      • FIG. 3B illustrates a sectional view of the related art turbofan in FIG. 2;
      • FIG, 4 illustrates another example of a related art turbofan;
      • FIG. 5 illustrates a section of a turbofan for explaining a state the turbofan is formed in a mold;
      • FIG. 6 illustrates a section showing an air flow when the turbofan in FIG. 4 is applied;
      • FIG. 7 illustrates a perspective view of a turbofan for use in a window air conditioner in accordance with a first preferred embodiment of the present invention;
      • FIG. 8 illustrates a section of the turbofan in FIG. 7;
      • FIG. 9 illustrates an enlarged view of key parts of the turbofan in FIG. 7;
      • FIG. 10 illustrates a section showing an air flow when the turbofan in accordance with a first preferred embodiment of the present invention is applied thereto;
      • FIGS. 11A and 11B illustrate sections of blades applicable to the embodiments of the present invention.
    DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
  • Reference will now be made in detail to the preferred embodiments of the present invention, examples of which are illustrated in the accompanying drawings. A turbofan in a window air conditioner in accordance with a first preferred embodiment of the present invention will be explained, with reference to FIGS. 7 - 10. FIG. 7 illustrates a perspective view of a turbofan for use in a window air conditioner in accordance with a first preferred embodiment of the present invention, FIG. 8 illustrates a section of the turbofan in FIG. 7, FIG. 9 illustrates an enlarged view of key parts of the turbofan in FIG. 7, and FIG. 10 illustrates a section showing an air flow when the turbofan in accordance with a first preferred embodiment of the present invention is applied thereto.
  • The turbofan in a window air conditioner in accordance with a first preferred embodiment of the present invention includes a base plate 30 having a hub 32 at a center thereof for coupling to a shaft of a driving motor, a plurality of blades 40 disposed at a periphery of the base plate 30 at fixed intervals along a circumferential direction, and a shroud 50 having an inlet side end part 52 formed in parallel to the shaft, fitted to ends of the blades 40 to connect the ends, with an inside diameter D1 equal to, or greater than an outside diameter D2 of the base plate 30, a shoulder part 54 extended outward in a radial direction from an inside circumference of the inlet side end part 52, and a sloped part 56 extended outward in a radial direction, and sloped downward, from an end of the shoulder part 54.
  • The base plate 30 has a central part with the hub 32 formed like a cap so that the central part is disposed near to an inlet compared to a bottom part 31 thereof on an outer side of the central part, for balancing a weight of the turbofan, wherein a connecting part 36 between the central part having the hub 32 and the bottom part 31 has a plurality of openings 38 along a circumference thereof for smooth discharge of a heat generated at the motor. It is preferable that a part the central part with the hub and the connecting part meet is curved, while the connecting part 36 is parallel to the shaft. A width of the shoulder part 54 of the shroud 50 is designed to be at least 4mm.
  • A mold for forming the turbofan in accordance with a first preferred embodiment of the present invention, and works of the turbofan formed from the mold will be explained.
  • The base plate 30, the blades 40, and the shroud 50 of the turbofan of the present invention are formed as one unit. A part that causes the greatest problem in the molds 'A' and 'B' of the foregoing structured turbofan is the shroud part 50. Therefore, as shown in FIG. 9, the upper mold 'A' is fitted such that the upper mold 'A' can be drawn through an inside diametral surface of the inlet side end part 52 of the shroud 50 after the turbofan is formed, and the lower mold 'B' is fitted such that the lower mold 'B' can be drawn to a lower side of the shoulder part 54 and the sloped part 56 along an out side diameter of the base plate 30 after the turbofan is formed. That is, a parting line of the molds is either on an outside diameter D2 of the base plate 30, or on an inside circumference of the inlet side end part 52 which has a greater diameter than the outside diameter D2.
  • Thus, the first preferred embodiment of the present invention permits to form the entire turbofan as one unit by one time of injection molding, since there is no overlapped part between the shroud 50 and the base plate 30, permitting to minimizing the defect ratio occurred in formation of the turbofan, that improves a productivity.
  • Moreover, the hub 32 on the base plate 30 disposed at a center part both in an axis direction and the radial direction can balance the turbofan, to allow stable and safe dismantling of the mold in formation of the turbofan, that prevents distortion of the turbofan. Moreover, the hub 32 at a center both in the axis direction and the radial direction permits to maintain balance when the hub is coupled to the shaft of the motor, such that the turbofan rotates accurately without eccentricity, which reduces vibration and noise.
  • In the meantime, the shroud 50 has the inlet side end part 52 parallel to the rotation axis, the shoulder part 54 extended outward from the inlet side end part 52 parallel to the base plate 30, and the sloped part 56 extended outward, and sloped with respect to the base plate 30, from a fore end the shoulder part 54. That is, the shoulder part 54 is annular with a depth 5 outwardly from the inlet side end part 52, to form a diameter D4 of an outer end of the shoulder part to be at least greater than an outside diameter D3 of the inlet side end part 52 of the shroud 50.
  • Referring to FIG. 10, the turbofan in accordance with a first preferred embodiment of the present invention has flow characteristics as shown in FIG. 10 owing to this configuration, resulting to reduce noise. That is, a noise caused by turbulence occurred at the shroud 50 is reduced. FIG. 10 illustrates an LDV experiment for visualizing a flow characteristic of the turbofan of the present invention, wherein a size of the turbulence occurred at the shroud 50 of the turbofan and characteristics of a discharge flow are shown. That is, the turbofan in accordance with a first preferred embodiment of the present invention has a good air flow characteristics, and especially, no vortex at the discharge side as shown in FIG. 10 owing to a configuration of the shroud 50. Therefore, in comparison to the related art, the turbofan of the present invention has lower noise if the air flow rates are the same. The greater death 'δ' of the shoulder part 54, which leads a width of a part of the lower mold 'B' for the shoulder 54 to be greater too, not only facilitates an easier fabrication of the molds 'A' and 'B' than the related art, but also inhibits wear to the maximum, to prolong the lifetime. That is, since the fist embodiment turbofan of the present invention can reduce noise for the same air flow rate, permit an easy formation of the molds; and inhibit wear relative to the related art, a lifetime of the molds can be increased.
  • FIGS. 11A and 11B illustrate sections of blades applicable to the embodiments of the present invention. The blades 40 and 60 of the turbofan in different embodiments of the present invention may have a streamlined section as shown in FIG. 11A, or a simple planar section as shown in FIG. 11B.
  • As has been explained, the turbofan in a window air conditioner of the present invention has the following advantages.
  • Unitary formation of a turbofan is facilitated to minimize a ratio of defects occurred in formation of the turbofan and to improve a productivity, an easy formation of a turbofan mold is made possible, and a lifetime of the mold is prolonged. Vibration and noise occurred during operation of the turbofan can be minimized.
  • It will be apparent to those skilled in the art that various modifications and variations can be made in the turbofan in an air conditioner of the present invention without departing from the scope of the invention. Thus, it is intended that the present invention cover the modifications and variations of this invention provided they come within the scope of the appended claims.

Claims (7)

  1. A turbofan for an air conditioner comprising:
    a base plate (30) having a hub (32) at a center thereof, the hub (32) coupled to a shaft of a driving motor;
    a plurality of blades (40) disposed at a periphery of the base plate (30) at fixed intervals along a circumferential direction; and,
    a shroud (50) including;
    an inlet side end part (52) formed in parallel to the shaft, and fitted to ends of the blades (40) to connect the ends, having an inside diameter equal to, or greater than an outside diameter of the baseplate (30),
    a shoulder part (54) extended outward in a radial direction from an inside circumference of the inlet side end part (52) parallel to the base plate (30), and
    a sloped part (56) extended outward in a radial direction, and sloped downward with respect to the base plate (30), from an end of the shoulder part (54).
  2. A turbofan as claimed in claim 1, wherein the base plate (30) includes;
    a central part having the hub (32) formed like a cap so that the central part is disposed near to an inlet compared to a bottom part (31) thereof on an outer side of the central part, and
    a connecting part (36) between the central part having the hub (32) and the bottom part (31) having a plurality of opening (38) along a circumference thereof.
  3. A turbofan as claimed in claim 2, wherein the connecting part (36) is parallel with a direction of the shaft, wherein a part where the central part and the connecting part (36) meet is curved.
  4. A turbofan as claimed in claim 1, wherein the shoulder part (54) has a at least 4mm width.
  5. A turbofan as claimed in claim 1, wherein the blade (40) has a streamlined or planar section.
  6. A turbofan as claimed in claim 1, wherein the blades (40) are given a slope to an upward base plate (30).
  7. A turbofan as claimed in claim 1, wherein the sloped part (56) is a rounded shape.
EP01307539A 2000-09-05 2001-09-05 Turbofan for air conditioner Expired - Lifetime EP1184575B1 (en)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
KR2000052278 2000-09-05
KR1020000052278A KR20020019154A (en) 2000-09-05 2000-09-05 Turbofan for air conditioner
KR10-2000-0052277A KR100389395B1 (en) 2000-09-05 2000-09-05 Turbofan for air conditioner
KR2000052277 2000-09-05
KR10-2001-0021435A KR100420355B1 (en) 2001-04-20 2001-04-20 Turbo fan in air-conditioner
KR2001021435 2001-04-20

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EP1184575A2 EP1184575A2 (en) 2002-03-06
EP1184575A3 EP1184575A3 (en) 2002-05-22
EP1184575B1 true EP1184575B1 (en) 2011-06-01

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Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100355827B1 (en) * 2000-08-17 2002-11-07 엘지전자 주식회사 Turbo fan of Window type Air conditioner
US6848887B2 (en) * 2001-08-23 2005-02-01 Lg Electronics Inc. Turbofan and mold thereof
US20030133801A1 (en) * 2002-01-15 2003-07-17 Orocio Reuel S. Impeller and method of manufacturing same
CN100414117C (en) * 2003-08-25 2008-08-27 乐金电子(天津)电器有限公司 Turbofan for air conditioner
TWI233469B (en) * 2004-02-03 2005-06-01 Delta Electronics Inc Fan assembly and impeller thereof
JP3879764B2 (en) * 2004-07-14 2007-02-14 ダイキン工業株式会社 Centrifugal blower
JP4581992B2 (en) * 2004-07-14 2010-11-17 ダイキン工業株式会社 Centrifugal blower and air conditioner equipped with the centrifugal blower
KR100824149B1 (en) * 2004-07-14 2008-04-21 다이킨 고교 가부시키가이샤 Centrifugal blower and air conditioner with centrifugal blower
CN100383402C (en) * 2004-07-19 2008-04-23 建准电机工业股份有限公司 Blast fan impeller harving blade radical length increasing air from side edge to bottom edge
CA2602068C (en) * 2005-03-29 2011-07-12 Carrier Corporation Single piece nozzle cover design and method of manufacture
EP1940496B1 (en) * 2005-10-28 2016-02-03 ResMed Motor Technologies Inc. Single or multiple stage blower and nested volute(s) and/or impeller(s) therefor
US9004067B2 (en) * 2005-10-28 2015-04-14 Redmed Limited Single or multiple stage blower and nested volute(s) and or impeller(s) thereof
EP3667093A1 (en) * 2006-05-24 2020-06-17 ResMed Motor Technologies Inc Compact low noise efficient blower for cpap devices
JP5026010B2 (en) * 2006-07-19 2012-09-12 デンヨー株式会社 Cooling fan for rotating equipment
EP1984683A4 (en) * 2006-10-19 2015-09-16 Lg Electronics Inc Turbo fan for blowing and refrigerator having the same
CN101377206B (en) * 2007-08-31 2013-08-07 富准精密工业(深圳)有限公司 Fan vane structure and centrifugal fan having the same
JP2010064825A (en) * 2008-09-09 2010-03-25 Toshiba Tec Corp Printer
JP2010196694A (en) * 2009-01-30 2010-09-09 Sanyo Electric Co Ltd Centrifugal blower and air conditioning device
JP2011174385A (en) * 2010-02-23 2011-09-08 Nippon Densan Corp Impeller and centrifugal fan
CN102466311B (en) * 2010-11-18 2016-04-27 乐金电子(天津)电器有限公司 Water fetching structure and use the window air conditioner of this structure
US10914316B1 (en) * 2011-08-23 2021-02-09 Climatecraft, Inc. Plenum fan
JP6155544B2 (en) 2012-03-12 2017-07-05 日本電産株式会社 Centrifugal fan
KR102076684B1 (en) * 2013-02-21 2020-02-12 엘지전자 주식회사 turbo fan and ceiling type air conditioner using it
US10184488B2 (en) 2013-02-25 2019-01-22 Greenheck Fan Corporation Fan housing having flush mounted stator blades
US10125783B2 (en) 2013-02-25 2018-11-13 Greenheck Fan Corporation Fan assembly and fan wheel assemblies
CN105392997B (en) 2013-02-25 2018-07-10 格林瀚克通风设备有限公司 Flow-mixing blower fan component
KR101645178B1 (en) 2013-05-10 2016-08-03 엘지전자 주식회사 Centrifugal fan and manufacturing method thereof
KR101577875B1 (en) * 2013-12-30 2015-12-28 동부대우전자 주식회사 Centrifugal fan for refrigerator
JP5884844B2 (en) * 2014-02-21 2016-03-15 株式会社ノーリツ Water heater
WO2016067409A1 (en) * 2014-10-30 2016-05-06 三菱電機株式会社 Turbofan, and indoor unit for air conditioning device
KR102289384B1 (en) * 2014-12-18 2021-08-13 삼성전자주식회사 Centrifugal fan assembly
CN107667225A (en) * 2015-05-22 2018-02-06 三星电子株式会社 Turbofan and the air regulator including turbofan
US10844876B2 (en) * 2015-06-16 2020-11-24 ResMed Pty Ltd Impeller with inclined and reverse inclined blades
KR20170009323A (en) * 2015-07-16 2017-01-25 이래오토모티브시스템 주식회사 Blower fan and blower including the same for air conditioner
CN105570197A (en) * 2016-02-18 2016-05-11 太仓钰丰机械工程有限公司 Silicone oil fan clutch with wind tunnel fan blades
USD949315S1 (en) * 2016-06-24 2022-04-19 Ebm-Papst Mulfingen Gmbh & Co. Kg Vane damper with trailing edge
DE102016111830A1 (en) * 2016-06-28 2017-12-28 Ebm-Papst Mulfingen Gmbh & Co. Kg Blower wheel and impeller
CN106089775B (en) * 2016-08-18 2018-12-07 北京超同步伺服股份有限公司 For cooling down the unilateral support blade blower of motor
CN106089776B (en) * 2016-08-18 2019-04-23 北京超同步伺服股份有限公司 The support construction of servo motor cooling blower
JP2018053804A (en) * 2016-09-29 2018-04-05 日本電産テクノモータ株式会社 Air blower
JP2018127952A (en) * 2017-02-08 2018-08-16 シナノケンシ株式会社 Air blower
CN107781213A (en) * 2017-10-19 2018-03-09 卧龙电气集团股份有限公司 A kind of circulating fan and its blade structure
JP2018071551A (en) * 2017-12-27 2018-05-10 日本電産株式会社 Centrifugal fan
CN111601972B (en) * 2018-01-19 2022-09-23 概创机械设计有限责任公司 Turbine with separate collectors
US11519421B2 (en) * 2018-07-06 2022-12-06 Zhongshan Broad-Ocean Motor Co., Ltd. Wind wheel and blower comprising the same
JP7240130B2 (en) * 2018-10-18 2023-03-15 株式会社荏原製作所 impeller used in pump
BE1027145B1 (en) * 2019-03-25 2020-10-27 Amotec Nv ROTOR FOR AN INDUSTRIAL FAN
GB2602987B (en) * 2021-01-22 2023-01-11 Cool T Ltd Fan apparatus and method of use
CN114474558B (en) * 2021-12-31 2024-04-26 太仓市福鑫防腐设备有限公司 Centrifugal ventilator impeller and integral injection molding manufacturing method thereof
JPWO2024009353A1 (en) * 2022-07-04 2024-01-11
CN116123109B (en) * 2023-04-04 2023-06-23 伦登风机科技(天津)有限公司 Involute blade type high-pressure fan

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4120170A (en) * 1977-04-04 1978-10-17 Carrier Corporation Apparatus for reducing condensate noise in an air conditioner
US4394111A (en) * 1981-09-11 1983-07-19 Snyder General Corporation Top cover, motor, fan and fan shroud assembly for an air conditioning unit
KR900005205Y1 (en) * 1985-07-01 1990-06-15 산요덴끼 가부시기가이샤 Air conditioner
JPH055536A (en) * 1990-11-07 1993-01-14 Daikin Ind Ltd Air conditioner
US5352089A (en) 1992-02-19 1994-10-04 Nippondenso Co., Ltd. Multi-blades fan device
JP2985656B2 (en) * 1994-04-26 1999-12-06 株式会社デンソー Centrifugal multi-blade fan and its manufacturing method
JPH09229409A (en) * 1996-02-22 1997-09-05 Sanyo Electric Co Ltd Air supply device and ceiling-embedded air conditioner using air supply device
KR980003248A (en) * 1996-06-25 1998-03-30 구자홍 Fan shroud of air conditioner outdoor unit
JP3285505B2 (en) * 1996-11-20 2002-05-27 東芝キヤリア株式会社 Fan motor mounting structure for ceiling cassette type air conditioner
JPH10153193A (en) * 1996-11-22 1998-06-09 Daikin Ind Ltd Turbofan
AU708393B2 (en) * 1997-06-17 1999-08-05 Daikin Industries, Ltd. Air conditioner
FR2772437B1 (en) 1997-12-11 2000-02-25 Valeo Climatisation MOTOR-FAN GROUP, PARTICULARLY FOR MOTOR VEHICLE HEATING AND AIR-CONDITIONING INSTALLATION
JPH11190537A (en) * 1997-12-26 1999-07-13 Daikin Ind Ltd Indoor machine for air-conditioner
KR100299823B1 (en) * 1998-01-20 2001-11-22 윤종용 Duct for window air conditioner
JP3500292B2 (en) * 1998-01-30 2004-02-23 日本電産コパル株式会社 Axial fan
JP3045159B2 (en) * 1998-02-27 2000-05-29 ダイキン工業株式会社 Indoor unit of air conditioner and installation structure of the indoor unit
US6042335A (en) * 1998-05-04 2000-03-28 Carrier Corporation Centrifugal flow fan and fan/orifice assembly
US6092988A (en) 1998-07-06 2000-07-25 Ford Motor Company Centrifugal blower assembly with a pre-swirler for an automotive vehicle

Also Published As

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JP2002156128A (en) 2002-05-31
US6679682B2 (en) 2004-01-20
EP1184575A2 (en) 2002-03-06
EP1184575A3 (en) 2002-05-22
CN1159531C (en) 2004-07-28
JP2006349343A (en) 2006-12-28
JP3907983B2 (en) 2007-04-18
CN1341813A (en) 2002-03-27
US20020028138A1 (en) 2002-03-07

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